2106 rev c - cooper · pdf filedocument 2106 rev. c instruction manual style 3, inset runway...

DOCUMENT 2106

REVISION C November 22, 2010

Instruction Manual

Style 3, Inset Runway Guard Light (SBGL), L-852G Style 3, Inset Runway Stop Bar Light (SBGL), L-852S

Style 3, Inset Stop Bar/Runway Guard Light (SBGL), L-852GS

Cooper Industries Crouse-Hinds Division Airport Lighting Products 1200 Kennedy Road Windsor, CT 06095

Copyright © 2010 Cooper Technologies Company

For Parts or Technical Service Call (860) 683-4300

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Instruction Manual

Style 3, Inset Runway Guard Light L-852G Style 3, Inset Stop Bar Light L-852S

Style 3, Inset Stop Bar/Runway Guard Light L-852GS

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1 Revisions REV. DESCRIPTION LTR. CHK. APV

A Initial Issue A201-210

KSS JMM

B Updated various text and parts list items for filter & filter bracket & lens, wedge filter and wedge filter bracket information. Copyright revised to 2010. FAA AC 150/5345-46D applied to this light sets.

A210-058

5/20/10 PG

C Figure 13, View A, rotated item 23 - 180 degrees A210- 241

11/22/10 PG

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2 Limited Product Warranty

THE FOLLOWING WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT BY WAY OF LIMITATION, ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR ANY PARTICULAR PURPOSE. Crouse-Hinds Airport Lighting Products (the “Company”) warrants to each original Buyer of Products manufactured by the Company that such Products are, at the time of delivery to the Buyer, free of material and workmanship defects, provided that no warranty is made with respect to: (a) any Product which has been repaired or altered in such a way, in Company’s judgment, as to

affect the Product adversely; (b) any Product which has, in Company’s judgment, been subject to negligence, accident or

improper storage; (c) any Product which has not been operated and maintained in accordance with normal practice

and in conformity with recommendations and published specification of Company; and, (d) any Products, component parts or accessories manufactured by others but supplied by

Company (any claims should be submitted directly to the manufacturer thereof). Crouse-Hinds Airport Lighting Products’ obligation under this warranty is limited to use of reasonable efforts to repair or, at its option, replace, during normal business hours, at any authorized service facility of Company, any Products which in its judgment proved not to be as warranted within the applicable warranty period. All costs of transportation of Products claimed not to be as warranted and of repaired or replacement Products to or from such service facility shall be borne by Purchaser. Company may require the return of any Product claimed not to be as warranted to one of its facilities as designed by Company, transportation prepaid by Purchaser, to establish a claim under this warranty. The cost of labor for installing a repaired or replacement product shall be borne by Purchaser. Replacement parts provided under the terms of this warranty are warranted for the remainder of the warranty period of the Products upon which they are installed to the same extent as if such parts were original components thereof. Warranty services provided under the Agreement does not assure uninterrupted operations of Products; Company does not assume any liability for damages caused by any delays involving warranty service. The warranty period for the Products is 24 months from date of shipment or 12 months from date of first use whichever occurs first.

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3 Safety Notices

NOTICE: NOTICE

This equipment is normally used or connected to circuits that may employ voltages that are dangerous and may be fatal if accidentally contacted by operating or maintenance personnel. Extreme caution should be exercised when working with this equipment. While practical safety precautions have been incorporated in this equipment, the following rules must be strictly observed.

3.1 Keep Away from Live Circuits

DANGER:

DANGER Operating and maintenance personnel must at all times observe all safety regulations. Do not perform maintenance on internal components or re-lamp with power ON.

3.2 Resuscitation

Maintenance personnel should familiarize themselves with the technique for resuscitation found in widely published manuals of first aid instructions.

IMPORTANT: IMPORTANT See FAA Advisory Circular AC 150/5340-26 for additional information.

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4 SAFETY SYMBOLS

DANGER:

DANGER The hazard or unsafe practice will result in severe injury or death.

WARNING:

WARNING The hazard or unsafe practice could result in severe injury or death.

CAUTION:

CAUTION The hazard or unsafe practice could result in minor injury.

NOTICE: NOTICE Possibly dangerous situation, goods might be damaged.

IMPORTANT: IMPORTANT Helpful information.

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5 Table of Contents

Title Page i 1 Revisions ii 2 Limited Product Warranty iii 3 Safety Notices iv 4 Safety Symbols v 5 Table of Contents vi 6 Part Number Explanation – Inset Runway and Stop Bar Light, L-852G & S 1 7 General Description 2 7.1. Inset Runway Guard Light, L-852G 2 7.2 Inset Stop Bar Light, L-852S 3 7.3 Combination Inset Stop Bar / Runway Guard Light, L-852GS 3 8 Installation 5 9 Maintenance 5 9.1 Cleaning Lenses 5 9.2 Relamping 6 9.3 Gasket Replacement 8 9.4 Lens Replacement 9 9.5 Feed-thru Replacement 9 9.6 Pressure Test 10 9.7 Cleanliness and Workmanship 10 9.8 Maintenance Program 10 11 Parts List 13 Figure 1 Lamp Bracket Orientation (852GS3-YX-P1) 2 Figure 2 Lamp Bracket Orientation (852GS3-XR-P1) 3 Figure 3 Lamp Bracket Orientation (852GS3-YR-P2) 4 Figure 4 Dual-lead wiring diagram (852GS3-YR-P2) 7 Figure 5 Single-lead wiring diagram (852GS3-XR-P1) 7 Figure 6 Single-lead wiring diagram (852GS3-YX-P1) 8 Figure 7 L-852G Wedge Filter Bracket Assembly 11 Figure 8 19999 Installation (Lifting) Tool 12 Figure 9 Top View of Fixture 16 Figure 10 Side View of Fixture 16 Figure 11 Feed-thru adapter detail 17 Figure 12 Bottom View of Fixture 17 Figure 13 Cut-away View of Fixture, L-852S 18 Figure 14 Cut-away View of Fixture, L-852G 19

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6 Part Number Explanation – Inset Runway and Stopbar Light, L-852G & S

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7 General Description 7.1 Inset Runway Guard Light, L-852G

The Crouse-Hinds Style 3 Inset Runway Guard Light is an ITS verified FAA L-852G per FAA AC 150/5345-46D. It is designed for installation at the intersection of taxiways and runways where visual guidance of moving aircraft is desirable. The fixture is designed to fit on a FAA L-868, steel, Size B light base per FAA AC 150/5345-42(latest version), and have a total height above grade/ground level of .250 inch. The fixture is unidirectional. It is weatherproof and will endure roll over loads without damage. The light fixture consists of a ductile iron support ring and a removable aluminum optical assembly. The ductile iron ring is mounted to a light base with six bolts (3/8-16 UNC x 1½ lg., stn. stl.) and lock washers (3/8, stn. stl.). The aluminum optical housing is secured to the ductile iron ring using two bolts, (3/8-16 UNC x 1½ lg., stn. stl.) and lock washers (3/8, stn. Stl) and two, high-strength shear pins. The optical housing has a die cast inner cover housing that is attached using 4 screws. A polyurethane o-ring is used to provide a watertight seal between the inner cover and optical housing (See Section 9.3). An optional silicone gasket is bonded to the outside of the inner cover to provide a watertight seal between the optical assembly and the ductile iron support ring. A 105-watt, MR-16 lamp is secured to a bracket, which is fastened to the bottom housing. Electrical connections are made at a feed-thru assembly in the inner cover. The feed-thru has an ITS verified L-823 plug for connecting to an FAA L-830/ L-831 Isolation Transformer. The lens is held in the aluminum housing with a bracket, gasket, molded elastomeric boot and two screws. There is a wedged shaped glass filter with fresnel lensing mounted to the optical housing between the lamp and lens. The light beam color is traffic signal yellow. All hardware is type 18-8 stainless steel. The complete light unit is 11.94 inches in diameter, 3.56 inches deep, and weighs 11 lbs.

Figure 1: Lamp Bracket Orientation – 852GS3-YX-P1

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7.2 Inset Stop Bar Light, L-852S

The Crouse-Hinds Inset Stop bar Light is an ITS verified FAA L-852S per FAA AC 150/5345-46D. Its design is identical to the L-852G described in section 8.5, with the following exceptions, the fresnel lens is mounted to the lens bracket, a traffic signal red filter is mounted to the lamp holder. Also the lamp, lamp bracket and Fresnel lens are mounted on the “A1” side of the bottom housing, as is the feed-thru adapter and assembly. The feed-thru adapter plug for this fixture is mounted on the “A2” side of the bottom of the housing. The lamp bracket orientation for this is shown below in Figure 2. Note that the lamp mounting bracket is mounted at the second hole back from the edge of the bottom housing. This allows for clearance for the Fresnel Wedge brackets mounted to the light housing.

Figure 2: Lamp Bracket Orientation – 852GS3-XR-P1 7.3 Combination Inset Stop Bar / Runway Guard Light, L-852GS The Crouse-Hinds Style 3 Inset Stop Bar / Runway Guard Light, 852GS3-YR-P2, is an ITS

verified combination FAA L-852G and L-852S per FAA AC 150/5345-46D. It is designed for installation at the intersection of taxiways and runways where visual guidance of moving aircraft is desirable. The fixture is designed to fit on a FAA L-868, steel, Size B light base per FAA AC 150/5345-42(latest version), and have a total height above grade/ground level of <.250 in. The fixture is unidirectional. It is weatherproof and will endure roll over loads without damage. The fixture is designed to fit on a FAA L-868, steel, Size B light base per FAA AC 150/5345-42(latest version), and have a total height above grade/ground level of <.250 in. The fixture is unidirectional. It is weatherproof and will endure roll over loads without damage. The aluminum light assembly is mounted to a light base with six bolts (3/8-16 UNC x 7/8 lg., stn. stl.) and lock washers (3/8, st. stl.) The aluminum housing has a die cast bottom housing that is attached using 6 screws. Two 105-watt, MR-16 lamps are secured to two brackets, which

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are fastened to the bottom housing, the lamp bracket orientation is shown below in Figure 3. Note that the lamp mounting bracket is mounted at the second hole back from the edge of the bottom housing. This allows for clearance for the Fresnel Wedge brackets mounted to the light housing. Electrical connections are made at two feed-thru assemblies in the inner cover. The feed-thru have an ITS verified L-823 plug for connecting to an FAA L-830/ L-831 Isolation Transformer. The lenses are held in the aluminum housing with a bracket, gasket, molded elastomeric boot and two screws per lens. The light beam color is traffic signal yellow on the left and traffic signal red on the right. All hardware is type 18-8 stainless steel. The complete light unit is 11.94 inches in diameter, 3.56 inches deep, and weighs 12 lbs. The fixture is designed to operate on two different circuits so that both lights cannot be on at the same time. More information on the circuits required for proper dual guard light/stop bar light operation can be found in FAA AC 150/5340-28.

Figure 3: Lamp Bracket Orientation – 852GS3-YR-P2

CAUTION:

CAUTION Never handle the light assembly by the leads as this can break the waterproof seal.

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8 INSTALLATION

The Style 3 SBGL light units are shipped complete, including the lamp(s), and are ready for installation as received. Installation of a light unit is to be done with primary POWER OFF and SECURED. At each SBGL light location, install a steel Size B, 12 inch deep minimum, L-868 Light Base per FAA AC 150/5340-4 (latest revision). For SBGL fixtures, install the light base with two opposite bolt holes parallel to the runway centerline. Place the properly sized isolation transformer(s) in the light base and make necessary primary power connections using L-823 connectors. The SBGL light unit requires either two 100 watt, 6.6A secondary transformers for the two lead version, or one 100 watt, 6.6A secondary transformer for the single lead version. Note that the two lead fixtures require two separate circuits for operation, so that the two circuits cannot be energized at the same time, see FAA AC 150/5340-28 for more information. Verify that the mounting flange on the light base is clean and the o-ring (optional on deep cans) is coated with Dow Corning FS 1292 grease and is in place on the light base. Connect the plug(s) from the light unit to the secondary (ies) of the previously installed isolation transformer(s). Installation tool, Crouse-Hinds P/N 19999, will ease in the installation and removal of the light unit (See Figure 6). The threaded eyebolts on the lifting tool screw into threaded holes in the light fixture. Lower the light unit straight down onto the base. The light fixture is subject to optical misalignment or mechanical damage if not seated properly. Verify the light beam(s)/color(s) are properly orientated for the individual location. Secure the light fixture to the base with six 3/8-16 UNC x 7/8 lg. stn. Stl. bolts and lock washers and tighten to 225 -0 +10 in-lbs. (18 ft-lbs.). It is recommended that Loctite 242 be used on the mounting bolts to prevent loosening due to vibration. It is highly recommended for fixtures subjected to repeated aircraft impacts and roll-overs.

9 MAINTENANCE

The preferred method of maintaining these lights is to periodically and systematically replace the Optical Assembly and return it to the maintenance shop for renovation. As an alternative, the Optical Assembly can be serviced in the field. However, it is recommended that field servicing be limited to cleaning the lens as described in section 9.1 and to lamp replacements as described in section 9.2.

9.1 Cleaning Lenses

With a compressed air blast or suitable brushes, remove all accumulated debris from the light channel. Clean the outer surface of the prism with a detergent solution. If the lens is coated with a substance impervious to the detergent, a suitable solvent should be sparingly applied with a wad of cotton or a patch of cloth on the end of a wood splint. After the solvent has acted the remaining solvent and softened coating should be removed with a clean piece of cotton or cloth. Care should be taken to avoid excessive contact between the solvent and the lens seal. Remove all remaining solvent from lens and seal. A gentle air blast may be used.

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9.2 Relamping

WARNING

WARNING Light assembly parts are hot when lamp is energized and remain hot for a short time after lamp/fixture is turned off.

Remove and secure power to the fixture. Separate the Optical Assembly from the outer ring by removing the two bolts. There are two pry slots in the optical housing to help separate the Optical Assembly from the support ring. Turn the Optical Assembly upside down and remove the four screws holding the inner cover to the light housing. Disconnect the lamp leads from the feed-thru terminals. Remove the Lamp Assembly by gently pulling up on the lamp reflector base. Inspect the feed-thru terminal for signs of corrosion. Replace feed-thru assemblies per paragraph 9.7. Clean the inside surfaces of the lens(es) with denatured alcohol. Inspect the lamp holder bracket(s) for loose hardware; tighten the mounting screws to 18 in-lbs., maximum.

CAUTION

CAUTION

Touching the quartz bulb with bare fingers may seriously shorten lamp life. If the bulb has been touched, wipe it clean with a piece of lens cleaning tissue or similar material moistened with denatured alcohol.

Install the new lamp by reversing the procedure above. Make certain the rim of the reflector is flush against the bracket and seated against the two pins at the bottom of the bracket. Position lamp, as shown in Figure 11. Connect the lamp leads to the feed-thru terminals and/or lamp jumpers. Refer to Figures 4, 5 and 6 for wiring detail. Inspect/ replace the inner cover o-ring per paragraph 9.5 (See Section 9.3). Assemble the inner cover onto the light housing. The screw hole patterns in the inner cover and light housing are offset to insure proper alignment. Tighten the mounting screws to 30 in-lbs. Perform a pressure test as described in paragraph 9.10. Reconnect the fixture plug(s) to the isolation transformer(s). Clean the mounting flange area of the support ring. Place the Optical Assembly into the support ring. Install new stainless steel, split-ring lock washers. Apply Loctite 242 (P/N 10048-30), per manufacturer’s instructions, to both mounting bolts and immediately torque them to 225 -0+10 in-lbs.

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Figure 4: Dual-lead wiring diagram (852GS3-YR-P2)

Figure 5: Single-lead wiring diagram (852GS3-XR-P1)

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Figure 6: Dual-lead wiring diagram (852GS3-YX-P1)

9.3 Gasket Replacement

Every time the Optical Assembly is opened the gasket must be closely examined and replaced if necessary. Any gasket that is stretched, torn, has a permanent set or some other defect, which would prevent it from forming a watertight seal, must be replaced with a new gasket. Remove the old gasket from the groove in the inner cover. Carefully clean the flange mating surfaces and the inner cover groove. This can be done by carefully scraping. Take care not to damage the mating surface and the bottom and sides of the groove. Coat the gasket (P/N 21140) with a thin layer of Dow Corning FS 1292 Lubricating grease. Position the new gasket in the center of the groove and press it into place. The groove is designed to be wider than the gasket, this provides room for displacement of the gasket when compressed between the housing load mating surfaces. The grease will hold the gasket in place while the inner cover is positioned on the light housing. Torque the inner cover screws to 30 in-lbs. Perform a pressure test as described in paragraph 9.10. Clean the mounting flange area of the support ring. Place the Optical Assembly into the support ring. Install new stainless steel, split-ring lock washers. Apply Loctite 242 (P/N 10048-30), per manufacturer’s instructions, to both mounting bolts and immediately torque them to 225 -0+10 in-lbs.

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9.4 Lens Replacement

If a lens is broken, leaks or is badly pitted or scarred, it must be replaced. It is highly recommended that this task be performed in a clean shop environment. Lens Replacement Kit P/N 21126-C contains all necessary parts to change a lens. Remove and secure power to the fixture. Separate the Optical Assembly from the outer ring by removing the two bolts. Turn the Optical Assembly upside down and remove the four screws holding the inner cover to the light housing. Remove the two lens retaining bracket screws from the light housing. Remove the lens-retaining bracket and discard the lens-retaining gasket. Firmly push the lens/boot assembly from the outside of the light housing; discard the old lens and boot. Thoroughly clean the lens opening with denatured alcohol and allow to dry. Inspect the lens opening for scratches or pits, a damaged lens opening surface will not seal properly. Place a new lens boot (P/N 21103) over the replacement lens (P/N 21102-X). Apply a thin coat of Dow Corning FS 1292 grease over the entire outside surface of the lens boot. Align the lens/boot assembly in the lens opening and press it into place. Verify that the lens boot is not pinched in the lens opening. Using a new lens retaining gasket (P/N 21101), fasten the lens retaining bracket (P/N 21100) to the light housing. Torque the mounting screws to 30 in-lbs. Assembly the inner cover onto the light housing. The screw hole patterns in the inner cover and light housing are offset to insure proper alignment. Torque the mounting screws to 30 in-lbs. Perform a pressure test per paragraph 9.10. Clean the mounting flange area of the support ring. Place the Optical Assembly into the support ring. Install new stainless steel, split-ring lock washers. Apply Loctite 242 (P/N 10048-30), per manufacturer’s instructions, to both mounting bolts and immediately torque them to 225 -0+10 in-lbs.

9.5 Feed-thru Replacement

Remove and secure power to the fixture. Separate the Optical Assembly from the outer ring by removing the two bolts. Turn the Optical Assembly upside down and remove the four screws holding the inner cover to the light housing. Disconnect the lamp leads from the feed-thru terminals. Remove the feed-thru by unscrewing the retaining collar. Clean the mounting surface with Isopropyl Alcohol and allow to dry. Apply a thin coat of Dow Corning FS 1292 grease to the mounting flange of a new feed-thru (P/N 21121 for 2 lamp/ 1 plug, or P/N 21122 for 1 lamp/ 1 plug). Apply a drop of Loctite 242 to the feed-thru adapter threads. Screw the feed-thru retaining collar onto the adapter; refer to Figure 8 for proper inner cover/ feed-thru orientation. Torque the retaining collar to 30 in-lbs. Assembly the inner cover onto the light housing. The screw hole patterns in the inner cover and light housing are offset to insure proper alignment. Torque the mounting screws to 30 in-lbs. Perform a pressure test per paragraph 9.10. Clean the mounting flange area of the support ring. Place the Optical Assembly into the support ring. Install new stainless steel, split-ring lock washers. Apply Loctite 242 (P/N 10048-30), per manufacturer’s instructions, to both mounting bolts and immediately torque them to 225 -0+10 in-lbs. placing in the support ring. Install new stainless steel, split-ring lock washers. Apply Loctite 242 (P/N 10048-30), per manufacturer’s instructions, to both mounting bolts and immediately torque them to 225 -0+10 in-lbs.

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9.6 Pressure Test

A light fixture should be subjected to a 20-psi air pressure test to verify that it is waterproof whenever it has been opened or components have been replaced. A tire valve style pressure fitting is located on the bottom of the inner cover. Pressurize the fixture to 20-psi then place it in a tub of water or use a soap solution to locate escaping air bubbles. Carefully inspect the areas around the lens, inner cover seal, and feed-thru adapter for leaks. Relieve the internal air pressure before installing the fixture or attempting to repair a leak.

WARNING:

WARNING

Do not exceed 20 psi when pressure testing the fixture. Serious injury and/or permanent damage to the fixture may result if a higher air pressure is used. Once the pressure test is complete be sure to relieve the air pressure.

9.7 Cleanliness and Workmanship

Service life depends upon the entire assembly being waterproof. All surfaces must be clean, dry and free of all foreign matter if the light fixture is to operate for extended periods without requiring maintenance.

9.8 Maintenance Program

In order to insure maximum light fixture life, the installed units should be subject to a maintenance program in accordance with the following: A daily operation check should be made of the lighting fixture. The lights should be energized and visually inspected. If any lamps are out, the location of the fixture should be recorded and the lamps replaced at a time when the circuit is de-energized. (See Section 9.2)

9.8.1 Regular cleaning is necessary in order to insure that inset lighting fixtures operate at maximum

efficiency. The lens and channel in front of the lens should be cleaned periodically with a soft cloth and solvent. The weather and the location of the fixtures will dictate the regularity and type of cleaning.

9.8.2 Snowplow operators should exercise extra care not to strike the light fixtures with snowplow

blades. After snowplow removal operations, inspect all light fixtures to locate and replace if necessary, any damaged Light Assemblies. Passes over the light rows should be made with a power broom only if practical. Whenever snowplows must traverse in-pavement light fixtures, they should be traveling at less than 5 mph or have the blades lifted clear of the fixtures. Recommended snow removal techniques are described in AC 150/5200-23.

9.8.3 The light is designed to exclude both ground and surface water from entering. If the lights are not

properly maintained (i.e., bolts tightened and seals in good condition) water may enter the fixture. To prevent this from occurring, it is recommended that each fixture be inspected for the presence

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of water at least once a month. More frequent inspection is desirable during and following rainy seasons

9.8.4 Optical Assembly and support ring hold-down bolts should be checked for proper torque (225 +5,

-0 in-lbs.) at least once every three months or whenever a fixture is serviced regardless of the season. Light fixtures in and around high speed exit areas are especially prone to vibration damage if the mounting bolts are not properly torqued. It is recommended that Loctite 242 be used on mounting bolts to prevent loosening due to vibration. The mounting surface of the light base must be clean and free of foreign matter when checking mounting bolts.

9.8.5 If any fixture contains water, the water should be removed and the entire fixture cleaned and

dried. Perform a pressure test per paragraph 9.10 to locate the source of the leak. Replace the bottom cover gasket, or optical housing o-ring, See Sections 9.3, 9.4 and 9.5.

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Figure 8: 19999 Installation (Lifting) tool TCL fixture shown

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10 PARTS LIST 10.1 Inset Runway Guard Light, L-852G

ITEM PART NUMBER 852GS3-YX-P1

QTY DESCRIPTION

1 21100 2 BRACKET, LENS RETAINING, 18-8 STN STL 2 21101* 1 GASKET, LENS RETAINING 3 21102-C* 2 LENS, CLEAR 4 21103* 2 BOOT, LENS 5 21137-11 1 OPTICAL HOUSING, MACHINED, REL, ALUMINUM 6 21461 1 LAMP BRACKET ASSEMBLY, 304 STN STL 7 21128 1 LAMP/REFLECTOR ASSEMBLY, 105W, 6.6A 8 21143* 1 GASKET, BLANK COLOR, LENS RETAINING 9 21138-1 1 BOTTOM COVER, MACHINED, REL, 1 PLUG, ALUM. 10 21120 1 ADAPTER, THREADED, FEED-THRU, ALUMINUM 11 21122 1 FEED-THRU ASSEMBLY, 1 LAMP/1/PLUG, ALUM. 12 10037-795 1 FITTING, PRESSURE TEST, 1/8 NPT 13 10048-25* A/R SILICONE GREASE 14 10048-106 A/R PIPE SEALANT 15 10035-61 1 O-RING, FEED-THRU 16 21109 1 FEED THRU PLUG 17 21148 1 BRACKET, LAMP MOUNTING 18 21129 1 BRACKET, FRESNEL WEDGE, L-852G 19 21131 1 SPRING CLIP, FRESNEL WEDGE BRACKET 20 21132 2 GASKET, FRESNEL WEDGE 21 21131 1 SPRING CLIP, FRESNEL WEDGE BRACKET 22 21130-TY 1 FRESNEL WEDGE, TRAFFIC SIGNAL YELLOW

23 N/A

24 N/A

25 10000-471 1 SCREW,SEMS, PAN HD TYPE 1A CROSS, GREEN, #10-32 X 3/8 LG, 18-8 STN STL

26 10000-468 4 SCREW,SEMS, PAN HD TYPE 1A CROSS/DRI-LOC, #10-32 X 1/2 LG, 18-8 STN STL


28 10000-400 6 SCREW,HEX WASHER HD/DRI-LOC, #10-32 X 3/8 LG, 18-8 STN STL

29 N/A 30 N/A 31 N/A 32 N/A

* - THESE PARTS ARE INCLUDED IN A LENS REPLACEMENT KIT. EACH KIT CONTAINS PARTS TO REPLACE ONE LENS

LENS COLOR

ITEM 3 PART NUMBER

LENS REPLACEMENT KIT PART NUMBER

CLEAR 21102-C 21126-C

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10.2 Inset Stop Bar Light, L-852S

ITEM PART NUMBER 852GS3-XR-P1

QTY DESCRIPTION

1 21100 2 BRACKET, LENS RETAINING, 18-8 STN STL 2 21101* 1 GASKET, LENS RETAINING 3 21102-C* 1 LENS, CLEAR 4 21103* 2 BOOT, LENS 5 21137-11 1 OPTICAL HOUSING, MACHINED, REL, ALUMINUM 6 21461 1 LAMP BRACKET ASSEMBLY, 304 STN STL 7 21128 1 LAMP/REFLECTOR ASSEMBLY, 105W, 6.6A 8 21143* 1 GASKET, BLANK COLOR, LENS RETAINING 9 21138-1 1 BOTTOM COVER, MACHINED, REL, 2 PLUG, ALUM. 10 21120 1 ADAPTER, THREADED, FEED-THRU, ALUMINUM 11 21122 1 FEED-THRU ASSEMBLY, 1 LAMP/1/PLUG, ALUM. 12 10037-795 1 FITTING, PRESSURE TEST, 1/8 NPT 13 10048-25* A/R SILICONE GREASE 14 10048-106 A/R PIPE SEALANT 15 10035-61 1 O-RING, FEED-THRU 16 21109 1 FEED THRU PLUG 17 21148 1 BRACKET, LAMP MOUNTING 18 21140 1 GASKET, BOTTOM COVER 19 N/A 20 21132 2 GASKET, FRESNEL WEDGE 21 N/A 22 N/A 23 21491 1 FRESNEL WEDGE, CLEAR, STOP BAR 24 21102-AR* 1 LENS, CLEAR, AR COATED




28 10000-400 6 SCREW,SEMS, HEX WASHER HD/DRI-LOC, #10-32 X 3/8 LG, 18-8 STN STL

29 N/A 30 21487 1 BRACKET, FRESNEL WEDGE, STOP BAR 31 21490 1 DICHROIC FILTER, RED, STOP BAR 32 21488 1 BRACKET, FILTER, STOP BAR


LENS COLOR ITEM 3

PART NUMBER LENS REPLACEMENT

KIT PART NUMBER CLEAR 21102-C 21126-C

CLEAR-AR COATED

21102-AR 21126-AR

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10.3 Combination Stop Bar / Runway Guard Light, L-852GS

ITEM PART NUMBER 852GS3-YR-P2

QTY DESCRIPTION

1 21100 2 BRACKET, LENS RETAINING, 18-8 STN STL 2 21101* 2 GASKET, LENS RETAINING 3 21102-C* 2 LENS, CLEAR 4 21103* 2 BOOT, LENS 5 21137-11 1 OPTICAL HOUSING, MACHINED, REL, ALUMINUM 6 21461 2 LAMP BRACKET ASSEMBLY, 304 STN STL 7 21128 2 LAMP/REFLECTOR ASSEMBLY, 105W, 6.6A 8 21143* 1 GASKET, BLANK COLOR, LENS RETAINING 9 21138 1 BOTTOM COVER, MACHINED, REL, 2 PLUG, ALUM. 10 21120 2 ADAPTER, THREADED, FEED-THRU, ALUMINUM 11 21122 2 FEED-THRU ASSEMBLY, 1 LAMP/1/PLUG, ALUM. 12 10037-795 1 FITTING, PRESSURE TEST, 1/8 NPT 13 10048-25* A/R SILICONE GREASE 14 10048-106 A/R PIPE SEALANT 15 10035-61 2 O-RING, FEED-THRU 16 N/A 17 21148 1 BRACKET, LAMP MOUNTING 18 21140 1 GASKET, BOTTOM COVER 19 21129 1 BRACKET, FRESNEL WEDGE, L-852G 20 21132 4 GASKET, FRESNEL WEDGE 21 21131 1 SPRING CLIP, FRESNEL WEDGE BRACKET 22 21130-TY 1 FRESNEL WEDGE, TRAFFIC SIGNAL YELLOW 23 21491 1 FRESNEL WEDGE, CLEAR, STOP BAR 24 21102-AR* 2 LENS, CLEAR, AR COATED




28 10000-400 6 SCREW,HEX WASHER HD/DRI-LOC, #10-32 X 3/8 LG, 18-8 STN STL

29 21158 1 BAFFLE 30 21487 1 BRACKET, FRESNEL WEDGE, STOP BAR 31 21490 2 DICHROIC FILTER, RED, STOP BAR 32 21488 1 BRACKET, FILTER, STOP BAR


LENS COLOR ITEM 3

PART NUMBER LENS REPLACEMENT

KIT PART NUMBER CLEAR-AR COATED

21102-AR 21126-AR

CLEAR 21102-C 21126-C

DOCUMENT 2106REV. C

Instruction Manual



16

Figure 9: Top View of Fixture

Figure 10: Side View of Fixture

DOCUMENT 2106REV. C

Instruction Manual



17

Figure 11: Feed-thru adapter Detail

Figure 12: Bottom View of Fixture

DOCUMENT 2106REV. C

Instruction Manual



18

Figure 13: Cut Away View of Fixture, L-852S

DOCUMENT 2106REV. C

Instruction Manual



19

Figure 14: Cut Away View of Fixture, L-852G

2106 rev c - cooper · pdf filedocument 2106 rev. c instruction manual style 3, inset runway...

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